Honeywell BENDIX/KING KLN 94 - Manual (Page 110)

B
KLN 94
Rev. 4, Jan/2003 10599I04.CDL Page B-2
FLIGHT MANUAL SUPPLEMENT PROCEDURE
For the installation of the KLN 94 GPS to be FAA approved for enroute and approach IFR
operation, it is necessary for the installer to create a flight manual supplement that is unique for
the installation and to submit that supplement to the FAA for approval.
Following, you will find a copy of the flight manual supplement created by Honeywell
International, Inc. for the initial STC installation of the KLN 94 in Mooney model M20C. Use this
supplement as a guide in creating the supplement for your installation (do not copy the 006- part
number in the footer). If your installation is interfaced to the same equipment (i.e. switches,
annunciators, RMI, autopilot, etc.) as the initial installation, copy the guide supplement in its
entirety, changing only the installers name and address, aircraft make and model, approval
authorization and section titles/numbers to suit your circumstances as detailed below. More likely,
if your installation is not identical to the initial installation, it will be necessary for you to determine
the differences and alter your supplement accordingly. Elements of the supplement which may
need to be altered for your installation are as follows:
1. FORMAT
The format of the finished supplement should match, as closely as possible, the format of the
aircraft’s flight manual and/or pilot’s operating handbook. Sizing of your manual to match the
aircraft’s flight manual is most easily accomplished by creating it first as an 8 1/2" X 11"
(standard typewriter size paper) document and then reducing that on a reducing copier to the
size required before submitting it to the FAA for approval. (Most small aircraft have flight
manuals of 5 1/2" X 8 1/2" size. This size has a different height/width ratio than the 8 1/2" X
11" size; the width is narrower. The guide supplement is proportioned correctly for reduction
to 5 1/2" X 8 1/2" size; copy its proportions if you are planning to reduce your supplement).
The headers and footers of the guide supplement may be rearranged to match the format of
your aircraft’s flight manual; however, most of the information shown is required on every
page. The Honeywell part number should not appear in your supplement, but the footer
should include the page number, in the format "PAGE _OF _", and the words "FAA
APPROVED" and a blank space for the date of the approval in place of the "ORIGINAL
ISSUE" of the guide supplement. The aircraft for which the supplement applies should also
be identified by manufacturer and model number as shown on the aircraft’s serial data plate,
i.e. Beech A36 or Piper PA-46-310P (not marketing name like Bonanza, Malibu, etc.).
Headers must identify the section of the supplement for that page. Additionally, we have
found it useful to include identification of the system in the header for ease of pilot reference.
The section numbers and names in the guide supplement are typical of many aircraft;
however, you should check the aircraft’s flight manual and match those section numbers and
names when organizing your supplement.